Zobrazeno 1 - 10
of 11
pro vyhledávání: '"Jean-Christophe Ehrstrom"'
Autor:
G. Salloum-Abou-Jaoude, Luc Salvo, Christophe Sigli, Frédéric De Geuser, Alexis Deschamps, Philippe Jarry, Jean-Christophe Ehrstrom
Publikováno v:
MATEC Web of Conferences, Vol 326, p 00001 (2020)
Publikováno v:
ICAF 2019 – Structural Integrity in the Age of Additive Manufacturing ISBN: 9783030215026
The current aircraft structures tend to increase the proportion of integral structure parts. One main advantage is the cost, through a reduction of the assembly complexity. The fatigue behaviour of integral structures is also improved due to a reduct
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::79d3b8af33fc6721aaef365612aec624
https://doi.org/10.1007/978-3-030-21503-3_27
https://doi.org/10.1007/978-3-030-21503-3_27
Publikováno v:
Materials Science and Technology. 20:567-576
This paper investigates the precipitation microstructures in aluminium alloys 7040 and 7050 (Al - Zn - Mg - Cu variants) as a function of quench rate and aging treatment, and the associated compromise between yield strength and fracture toughness. Th
Publikováno v:
Materials Science Forum. :2941-2946
Publikováno v:
Materials Science and Technology. 18:1085-1091
The fracture behaviour in tension of an Al-Mg -Mn alloy has been investigated. At high temperatures and strain rates, intergranular brittle fracture is observed along with cleavage fracture. Intergranular fracture is related to local melting at the g
Autor:
Jean-Christophe Ehrstrom, Ronan Dif
Publikováno v:
Materials Science Forum. :1285-1290
Publikováno v:
Materials Science and Engineering: A. :583-586
The fracture behavior of the 5383 aluminum alloy is investigated at high temperature (490–560 °C) and high strain rate (l0−2–25 s−1) by the secondary tensile test. A dramatic decrease of ductility is observed at all temperatures for the high
Publikováno v:
Materials Science Forum. :5-16
New aluminum alloys for aircraft structures have been introduced recently. These new alloys are designed in such a way as to improve the weight efficiency of the structure. A good understanding of the loading of the different airframe parts is needed
Autor:
Jean-Christophe Ehrstrom, Bernard Bes, Robert Dif, H. Mayet, H. Ribes, Christophe Sigli, Ph. Lassince
Publikováno v:
Materials Science Forum. :1613-1618
Alloys of the Al-Mg-Si-Cu series like AA6056 are good candidates for welded fuselage panels. The first part of the paper recalls the main metallurgical influences on final properties (mechanical strength, damage tolerance and intergranular corrosion
Publikováno v:
45th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conference.
An attempt was made to predict the variable amplitude fatigue crack growth performance of aluminium alloys using existing simulation software. The experimental basis for validation consisted of variable amplitude tests for a large transport wing spec